View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67952U 26145.58335647 +.00000000 +00000-0 -91282-3 0 00007
2 67952 42.9996 116.7031 0001286 264.7849 246.1156 15.27595175 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001286 |
| inclination: | 42.9996° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 116.7031° |
| argument of perigee: | 264.7849° |
| revolutions per day: | 15.27595175 |
| mean anomaly at epoch: | 246.1156° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|